GOE 424 AIRFOIL (goe424-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 424 AIRFOIL (goe424-il) Reynolds number: 500,000 Max Cl/Cd: 93.85 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe424-il-500000-n5.txt Download as CSV file: xf-goe424-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 424 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -0.7946 0.07276 0.06916 -0.0907 1.0000 0.0191
-17.500 -0.8131 0.06674 0.06302 -0.0941 1.0000 0.0193
-17.250 -0.8231 0.06227 0.05847 -0.0964 1.0000 0.0194
-17.000 -0.8305 0.05843 0.05456 -0.0983 1.0000 0.0196
-16.750 -0.8373 0.05503 0.05109 -0.0995 1.0000 0.0198
-16.500 -0.8439 0.05207 0.04806 -0.1001 1.0000 0.0199
-16.250 -0.8440 0.04921 0.04513 -0.1015 0.9988 0.0201
-16.000 -0.8346 0.04630 0.04213 -0.1045 0.9958 0.0204
-15.750 -0.8242 0.04356 0.03929 -0.1074 0.9931 0.0208
-15.500 -0.8157 0.04097 0.03659 -0.1096 0.9882 0.0212
-15.250 -0.8056 0.03842 0.03390 -0.1118 0.9838 0.0216
-15.000 -0.7968 0.03602 0.03133 -0.1134 0.9780 0.0221
-14.750 -0.7864 0.03379 0.02892 -0.1148 0.9714 0.0225
-14.500 -0.7733 0.03234 0.02742 -0.1155 0.9637 0.0228
-14.250 -0.7586 0.03112 0.02616 -0.1161 0.9561 0.0231
-14.000 -0.7462 0.03008 0.02507 -0.1158 0.9468 0.0233
-13.750 -0.7333 0.02912 0.02404 -0.1154 0.9374 0.0237
-13.500 -0.7211 0.02821 0.02305 -0.1146 0.9263 0.0240
-13.250 -0.7090 0.02730 0.02205 -0.1137 0.9138 0.0245
-13.000 -0.6972 0.02635 0.02098 -0.1126 0.8987 0.0250
-12.750 -0.6856 0.02536 0.01981 -0.1112 0.8798 0.0255
-12.500 -0.6735 0.02440 0.01862 -0.1097 0.8581 0.0261
-12.250 -0.6596 0.02376 0.01784 -0.1083 0.8342 0.0264
-12.000 -0.6441 0.02331 0.01725 -0.1070 0.8101 0.0267
-11.750 -0.6278 0.02295 0.01675 -0.1057 0.7865 0.0270
-11.500 -0.6112 0.02263 0.01629 -0.1044 0.7608 0.0274
-11.250 -0.5957 0.02233 0.01583 -0.1028 0.7329 0.0279
-11.000 -0.5801 0.02201 0.01532 -0.1011 0.7028 0.0284
-10.750 -0.5626 0.02158 0.01469 -0.0998 0.6758 0.0290
-10.500 -0.5442 0.02111 0.01401 -0.0986 0.6544 0.0296
-10.250 -0.5250 0.02065 0.01337 -0.0975 0.6383 0.0301
-10.000 -0.5050 0.02031 0.01296 -0.0965 0.6256 0.0305
-9.750 -0.4840 0.02005 0.01263 -0.0957 0.6148 0.0310
-9.500 -0.4624 0.01977 0.01228 -0.0949 0.6064 0.0314
-9.250 -0.4405 0.01948 0.01191 -0.0941 0.5983 0.0319
-9.000 -0.4184 0.01917 0.01151 -0.0934 0.5913 0.0325
-8.750 -0.3959 0.01881 0.01107 -0.0927 0.5848 0.0332
-8.500 -0.3736 0.01844 0.01058 -0.0919 0.5785 0.0338
-8.250 -0.3510 0.01809 0.01012 -0.0911 0.5732 0.0344
-8.000 -0.3285 0.01766 0.00968 -0.0904 0.5687 0.0349
-7.750 -0.3052 0.01738 0.00938 -0.0898 0.5640 0.0354
-7.500 -0.2818 0.01713 0.00908 -0.0892 0.5596 0.0359
-7.250 -0.2585 0.01685 0.00875 -0.0886 0.5557 0.0365
-7.000 -0.2347 0.01654 0.00840 -0.0880 0.5524 0.0370
-6.750 -0.2109 0.01624 0.00806 -0.0874 0.5488 0.0377
-6.500 -0.1869 0.01599 0.00775 -0.0868 0.5453 0.0384
-6.250 -0.1628 0.01576 0.00745 -0.0862 0.5419 0.0391
-6.000 -0.1400 0.01545 0.00709 -0.0855 0.5385 0.0396
-5.750 -0.1163 0.01515 0.00678 -0.0849 0.5357 0.0402
-5.500 -0.0919 0.01490 0.00652 -0.0844 0.5327 0.0408
-5.250 -0.0673 0.01468 0.00628 -0.0839 0.5298 0.0414
-5.000 -0.0426 0.01448 0.00605 -0.0834 0.5270 0.0422
-4.750 -0.0178 0.01430 0.00583 -0.0829 0.5244 0.0431
-4.500 0.0071 0.01415 0.00563 -0.0824 0.5220 0.0439
-4.250 0.0321 0.01401 0.00544 -0.0820 0.5196 0.0446
-4.000 0.0567 0.01374 0.00517 -0.0815 0.5177 0.0454
-3.750 0.0820 0.01354 0.00498 -0.0811 0.5154 0.0463
-3.500 0.1076 0.01339 0.00481 -0.0808 0.5130 0.0472
-3.250 0.1334 0.01325 0.00466 -0.0805 0.5105 0.0483
-3.000 0.1593 0.01315 0.00452 -0.0802 0.5082 0.0496
-2.750 0.1854 0.01307 0.00441 -0.0800 0.5061 0.0507
-2.500 0.2107 0.01292 0.00424 -0.0796 0.5041 0.0521
-2.250 0.2365 0.01284 0.00412 -0.0794 0.5022 0.0536
-2.000 0.2632 0.01275 0.00403 -0.0792 0.5005 0.0552
-1.750 0.2900 0.01267 0.00394 -0.0791 0.4986 0.0570
-1.500 0.3166 0.01258 0.00386 -0.0790 0.4965 0.0598
-1.250 0.3431 0.01251 0.00379 -0.0788 0.4944 0.0634
-1.000 0.3695 0.01243 0.00373 -0.0787 0.4926 0.0712
-0.750 0.3912 0.01186 0.00359 -0.0780 0.4908 0.2134
-0.500 0.4124 0.01129 0.00350 -0.0772 0.4890 0.3552
-0.250 0.4370 0.01110 0.00351 -0.0768 0.4871 0.4211
0.000 0.4625 0.01101 0.00353 -0.0765 0.4851 0.4639
0.250 0.4884 0.01092 0.00357 -0.0764 0.4834 0.5046
0.500 0.5145 0.01083 0.00363 -0.0762 0.4819 0.5442
0.750 0.5408 0.01077 0.00369 -0.0760 0.4801 0.5799
1.000 0.5671 0.01073 0.00375 -0.0759 0.4781 0.6102
1.250 0.5934 0.01071 0.00381 -0.0757 0.4761 0.6381
1.500 0.6195 0.01070 0.00388 -0.0755 0.4742 0.6673
1.750 0.6456 0.01070 0.00396 -0.0753 0.4723 0.6942
2.000 0.6715 0.01072 0.00404 -0.0751 0.4703 0.7183
2.250 0.6973 0.01075 0.00414 -0.0748 0.4683 0.7459
2.500 0.7230 0.01077 0.00426 -0.0745 0.4665 0.7748
2.750 0.7487 0.01078 0.00437 -0.0742 0.4646 0.8036
3.000 0.7741 0.01080 0.00450 -0.0738 0.4625 0.8302
3.250 0.7993 0.01084 0.00462 -0.0734 0.4603 0.8561
3.500 0.8244 0.01090 0.00474 -0.0729 0.4577 0.8787
3.750 0.8490 0.01098 0.00484 -0.0724 0.4545 0.8980
4.000 0.8736 0.01111 0.00495 -0.0719 0.4507 0.9151
4.250 0.9005 0.01119 0.00509 -0.0719 0.4470 0.9308
4.500 0.9295 0.01130 0.00522 -0.0724 0.4436 0.9451
4.750 0.9600 0.01143 0.00537 -0.0732 0.4408 0.9575
5.000 0.9906 0.01159 0.00552 -0.0742 0.4379 0.9687
5.250 1.0236 0.01178 0.00568 -0.0757 0.4349 0.9788
5.500 1.0600 0.01195 0.00588 -0.0779 0.4322 0.9873
5.750 1.0965 0.01211 0.00607 -0.0802 0.4292 0.9945
6.000 1.1335 0.01229 0.00627 -0.0827 0.4259 0.9996
6.250 1.1459 0.01237 0.00635 -0.0799 0.4230 1.0000
6.500 1.1588 0.01249 0.00646 -0.0773 0.4201 1.0000
6.750 1.1754 0.01264 0.00660 -0.0754 0.4171 1.0000
7.000 1.1951 0.01277 0.00678 -0.0742 0.4134 1.0000
7.250 1.2144 0.01294 0.00696 -0.0730 0.4091 1.0000
7.500 1.2329 0.01315 0.00717 -0.0717 0.4047 1.0000
7.750 1.2524 0.01338 0.00741 -0.0706 0.4002 1.0000
8.000 1.2725 0.01360 0.00766 -0.0696 0.3941 1.0000
8.250 1.2897 0.01392 0.00795 -0.0682 0.3877 1.0000
8.500 1.3094 0.01420 0.00826 -0.0673 0.3813 1.0000
8.750 1.3269 0.01456 0.00862 -0.0661 0.3742 1.0000
9.000 1.3444 0.01495 0.00901 -0.0649 0.3673 1.0000
9.250 1.3603 0.01542 0.00947 -0.0636 0.3587 1.0000
9.500 1.3754 0.01595 0.01000 -0.0622 0.3496 1.0000
9.750 1.3875 0.01663 0.01065 -0.0604 0.3397 1.0000
10.000 1.4012 0.01729 0.01130 -0.0590 0.3300 1.0000
10.250 1.4134 0.01805 0.01206 -0.0574 0.3217 1.0000
10.500 1.4237 0.01894 0.01295 -0.0557 0.3121 1.0000
10.750 1.4338 0.01991 0.01390 -0.0541 0.3023 1.0000
11.000 1.4403 0.02112 0.01509 -0.0523 0.2924 1.0000
11.250 1.4468 0.02240 0.01637 -0.0506 0.2823 1.0000
11.500 1.4527 0.02378 0.01776 -0.0490 0.2731 1.0000
12.000 1.4593 0.02715 0.02113 -0.0458 0.2547 1.0000
12.250 1.4593 0.02923 0.02321 -0.0443 0.2467 1.0000
12.500 1.4631 0.03110 0.02511 -0.0432 0.2391 1.0000
12.750 1.4614 0.03351 0.02754 -0.0419 0.2325 1.0000
13.000 1.4658 0.03549 0.02956 -0.0411 0.2269 1.0000
13.250 1.4660 0.03790 0.03201 -0.0403 0.2211 1.0000
13.500 1.4637 0.04061 0.03474 -0.0394 0.2161 1.0000
13.750 1.4669 0.04282 0.03701 -0.0388 0.2112 1.0000
14.000 1.4655 0.04551 0.03975 -0.0382 0.2058 1.0000
14.250 1.4612 0.04852 0.04278 -0.0375 0.2008 1.0000
14.500 1.4639 0.05085 0.04516 -0.0370 0.1959 1.0000
14.750 1.4618 0.05366 0.04801 -0.0365 0.1906 1.0000
15.000 1.4573 0.05676 0.05113 -0.0360 0.1858 1.0000
15.250 1.4592 0.05922 0.05365 -0.0357 0.1803 1.0000
15.500 1.4549 0.06237 0.05681 -0.0353 0.1741 1.0000
15.750 1.4531 0.06527 0.05975 -0.0351 0.1683 1.0000
16.000 1.4496 0.06837 0.06286 -0.0348 0.1609 1.0000
16.250 1.4456 0.07160 0.06611 -0.0347 0.1539 1.0000
16.500 1.4380 0.07526 0.06975 -0.0345 0.1452 1.0000
16.750 1.4313 0.07883 0.07332 -0.0344 0.1357 1.0000
17.000 1.4240 0.08252 0.07701 -0.0344 0.1277 1.0000
17.250 1.4168 0.08624 0.08072 -0.0345 0.1206 1.0000
17.500 1.4131 0.08960 0.08410 -0.0347 0.1145 1.0000
17.750 1.4065 0.09329 0.08780 -0.0349 0.1085 1.0000
18.000 1.4037 0.09658 0.09112 -0.0352 0.1030 1.0000
18.250 1.3966 0.10043 0.09497 -0.0356 0.0970 1.0000
18.500 1.3926 0.10394 0.09851 -0.0360 0.0899 1.0000
18.750 1.3858 0.10783 0.10239 -0.0366 0.0811 1.0000
19.000 1.3655 0.11353 0.10800 -0.0375 0.0619 1.0000
19.250 1.3439 0.11952 0.11392 -0.0386 0.0483 1.0000
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